Integrated guidance for Mars entry and powered descent using reinforcement learning and pseudospectral method-Reference-Cited by-同舟云学术

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Integrated guidance for Mars entry and powered descent using reinforcement learning and pseudospectral method

Published:2019-10 Issue: Volume:163 Page:114-129
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Jiang Xiuqiang^ORCID,Li Shuang^ORCID,Furfaro Roberto

Funder

National Natural Science Foundation of China

China Scholarship Council

Jiangsu Province

NUAA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. A rigid mid lift-to-drag ratio approach to human Mars entry, descent, and landing;Cerimele,2017

2. Mid-lift-to-drag ratio rigid vehicle control system design and simulation for human Mars entry;Johnson,2018

3. Adaptive powered descent initiation and fuel-optimal guidance for Mars applications;Lu,2018

4. The development of the MSL guidance, navigation, and control system for entry, descent, and landing;San Martin,2013

5. Propellant-optimal powered descent guidance;Lu;J. Guid. Contr. Dynam.,2018

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